ATL82FA035

NTSB accident investigation · Beech F50 · Picayune, MS · January 17, 1982

Accident · FatalField investigationFinal report
Date
January 17, 1982, 05:39 local (11:39 UTC)
Place
Picayune, MS
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N654TBeech F50
Weather
Visual (VMC) · Night/bright
Status
Completed · report January 17, 1983
Report
Approved by Office Director
FAA report
19820117001059A
Case key
72221

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfTakeoff - initial climb
Engine assembly,ring - wornFactor
Maintenance,annual inspection - not performedCompany/operator managementFactor
Acft/equip,inadequate compliance determinationCompany/operator managementFactor
Operation with known deficiencies in equipment - initiatedPilot in commandFactor
PressurePilot in commandFactor
Eng assembly,blower/impeller/integral supercharger - failure,partialCause
Fluid,oil - starvationCause
Eng assembly,blower/impeller/integral supercharger - failure,totalCause
Loss of control - in flightTakeoff - initial climb
Light condition - dark nightFactor
Emergency procedure - improperPilot in commandCause
QualificationPilot in commandCause
Lack of total experience in kind of aircraftPilot in commandCause
Airspeed(vmc) - not maintainedPilot in commandCause
Relinquishing of control - improperPilot in commandCause
Flt control syst,rudder control - failure,total
Directional control - not possibleCopilot/second pilot
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The aircraft took off during darkness with a single-engine pilot in the pilot-in-command (PIC) position and a multi-engine instructor pilot in the copilot (cp) position. The PIC had a full set of controls (when the yoke was on his side); however, there were no rudder pedals for the cp. After takeoff, the plane crashed in a nose low, 90 deg left bank, attitude. A witness reported that the propellers sounded like they were out of pitch during takeoff. The landing gear was found in the extended position. The yoke was found on the cp side. The left propeller blades were bent aft and 2 of the blades were found in the normal high pitch position. An examination of the left engine revealed 6 of 6 cylinders had low compression. The supercharger was worn, the impeller partially disintegrated from rubbing on its housing, and the impeller drive shaft was bent and had been overheated. The aircraft did not have a current annual inspection. There was evidence the PIC was under pressure to complete the itinerary.

Aircraft

Registration
N654T
Reported as
Beech F50
Category
Airplane
Serial number
FH-84
Airframe hours
2,866
Engine
Lycoming GSO-480-B1B6, 340 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Part 91
Operator
Mr. Rene Martin
Registered owner
Grant Equipment Company
Departed
PCU · Picayune, MS
Destination
Jamaica, OF
Airport
PCU · Picayune-Pearl River Cnty

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
53
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Flight hours
755 total

Weather

Conditions
Visual (VMC) · Night/bright
Temperature
73 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.